Airworthiness Directives; Bombardier Model CL600-1A11 (CL-600), Model CL-600-2A12 (CL-601), and Model CL-600-2B16 (CL-601-3A, CL-601- 3R, and CL-604) Series Airplanes, 28988 [C5-9186]

Download as PDF 28988 Corrections Federal Register Vol. 70, No. 96 Thursday, May 19, 2005 This section of the FEDERAL REGISTER contains editorial corrections of previously published Presidential, Rule, Proposed Rule, and Notice documents. These corrections are prepared by the Office of the Federal Register. Agency prepared corrections are issued as signed documents and appear in the appropriate document categories elsewhere in the issue. Monday, May 16, 2005, make the following correction: On page 26559, in the second column, following the signature block, the document line should read ‘‘[FR Doc. 8796 Filed 05–13–05; 8:45 am]’’. [FR Doc. C5–8796 Filed 5–18–05; 8:45 am] 4. On the same page, in the same section, in the same table, under the column Model, in the eighth entry remove the word ‘‘retraction.’’ [FR Doc. C5–9186 Filed 5–18–05; 8:45 am] BILLING CODE 1505–01–D BILLING CODE 1505–01–D DEPARTMENT OF TRANSPORTATION DEPARTMENT OF TRANSPORTATION ENVIRONMENTAL PROTECTION AGENCY Federal Aviation Administration 40 CFR Part 52 [R03–OAR–2004–DC–0007; FRL–7909–8] Approval and Promulgation of Air Quality Implementation Plans; District of Columbia; VOC Emission Standards for AIM Coatings Correction In rule document 05–9312 beginning on page 24959 in the issue of Thursday, May 12, 2005, make the following correction: §52.470 [Corrected] On pages 24969 and 24970, in §52.470, in the table, in the column ‘‘EPA approval date’’, ‘‘5/21/05’’ should read ‘‘5/12/05’’ throughout the column. [FR Doc. C5–9312 Filed 5–18–05; 8:45 am] BILLING CODE 1505–01–D REGULATORY INFORMATION SERVICE CENTER Introduction to the Unified Agenda of Federal Regulatory and Deregulatory Actions Correction In proposed rule document 05–8796 beginning on page 26555 in the issue of VerDate jul<14>2003 22:18 May 18, 2005 Jkt 205001 14 CFR Part 39 [Docket No. FAA-2005-21139; Directorate Identifier 2003-NM-196-AD] Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20356; Directorate Identifier 2004-NM-115-AD] RIN 2120-AA64 RIN 2120-AA64 Airworthiness Directives; Bombardier Model CL600–1A11 (CL–600), Model CL–600–2A12 (CL–601), and Model CL– 600–2B16 (CL–601–3A, CL–601–3R, and CL–604) Series Airplanes Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes Correction In proposed rule document 05–9186 beginning on page 24331 in the issue of Monday, May 9, 2005, make the following corrections: 1. On page 24332, in the table Messier-Dowty Service Bulletins, under the column Landing gear component, the seventh entry should read ‘‘MLG shock strut pin.’’ 2. On the same page, in the same table, under the column Corresponding Bombardier service bulletin(s), the seventh entry should read ‘‘601-0546.’’ In proposed rule document 05–2834 beginning on page 7693 in the issue of Tuesday, February 15, 2005, make the following corrections: §39.13 [Corrected] 3. On page 24334, in §39.13, in Table 2, under the column Messier-Dowty service bulletin, the last entry should read ‘‘M-DT SB7300–32–16, dated July 12, 2001.’’. PO 00000 Frm 00001 Fmt 4734 Sfmt 4734 Correction §39.13 [Corrected] 1. On page 7695, in the second column, in §39.13, after amendatory instruction 2, in the next line, ‘‘FAA– 20356’’ should read ‘‘FAA–2005– 20356.’’ 2. On the same page, in the third column, in the same section, under the heading Optional Terminating Action, in the first line, ‘‘(1)’’ should read ‘‘(i).’’ [FR Doc. C5–2834 Filed 5–18–05; 8:45 am] BILLING CODE 1505–01–D E:\FR\FM\19MYCX.SGM 19MYCX

Agencies

[Federal Register Volume 70, Number 96 (Thursday, May 19, 2005)]
[Corrections]
[Page 28988]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: C5-9186]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-21139; Directorate Identifier 2003-NM-196-AD]
RIN 2120-AA64


Airworthiness Directives; Bombardier Model CL600-1A11 (CL-600), 
Model CL-600-2A12 (CL-601), and Model CL-600-2B16 (CL-601-3A, CL-601-
3R, and CL-604) Series Airplanes

Correction

    In proposed rule document 05-9186 beginning on page 24331 in the 
issue of Monday, May 9, 2005, make the following corrections:
    1. On page 24332, in the table Messier-Dowty Service Bulletins, 
under the column Landing gear component, the seventh entry should read 
``MLG shock strut pin.''
    2. On the same page, in the same table, under the column 
Corresponding Bombardier service bulletin(s), the seventh entry should 
read ``601-0546.''


Sec. 39.13  [Corrected]

    3. On page 24334, in Sec. 39.13, in Table 2, under the column 
Messier-Dowty service bulletin, the last entry should read ``M-DT 
SB7300-32-16, dated July 12, 2001.''.
    4. On the same page, in the same section, in the same table, under 
the column Model, in the eighth entry remove the word ``retraction.''

[FR Doc. C5-9186 Filed 5-18-05; 8:45 am]
BILLING CODE 1505-01-D
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